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S17400 Stainless Steel vs. 772.0 Aluminum

S17400 stainless steel belongs to the iron alloys classification, while 772.0 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (7, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is S17400 stainless steel and the bottom bar is 772.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 11 to 21
6.3 to 8.4
Fatigue Strength, MPa 380 to 670
94 to 160
Poisson's Ratio 0.28
0.32
Shear Modulus, GPa 75
26
Tensile Strength: Ultimate (UTS), MPa 910 to 1390
260 to 320
Tensile Strength: Yield (Proof), MPa 580 to 1250
220 to 250

Thermal Properties

Latent Heat of Fusion, J/g 280
380
Maximum Temperature: Mechanical, °C 850
180
Melting Completion (Liquidus), °C 1440
630
Melting Onset (Solidus), °C 1400
580
Specific Heat Capacity, J/kg-K 480
870
Thermal Conductivity, W/m-K 17
150
Thermal Expansion, µm/m-K 11
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
35
Electrical Conductivity: Equal Weight (Specific), % IACS 2.6
110

Otherwise Unclassified Properties

Base Metal Price, % relative 14
9.5
Density, g/cm3 7.8
3.0
Embodied Carbon, kg CO2/kg material 2.7
8.0
Embodied Energy, MJ/kg 39
150
Embodied Water, L/kg 130
1140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140 to 160
16 to 25
Resilience: Unit (Modulus of Resilience), kJ/m3 880 to 4060
350 to 430
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
46
Strength to Weight: Axial, points 32 to 49
25 to 31
Strength to Weight: Bending, points 27 to 35
31 to 36
Thermal Diffusivity, mm2/s 4.5
58
Thermal Shock Resistance, points 30 to 46
11 to 14

Alloy Composition

Aluminum (Al), % 0
91.2 to 93.2
Carbon (C), % 0 to 0.070
0
Chromium (Cr), % 15 to 17
0.060 to 0.2
Copper (Cu), % 3.0 to 5.0
0 to 0.1
Iron (Fe), % 70.4 to 78.9
0 to 0.15
Magnesium (Mg), % 0
0.6 to 0.8
Manganese (Mn), % 0 to 1.0
0 to 0.1
Nickel (Ni), % 3.0 to 5.0
0
Niobium (Nb), % 0.15 to 0.45
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
0 to 0.15
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0.1 to 0.2
Zinc (Zn), % 0
6.0 to 7.0
Residuals, % 0
0 to 0.15